Orbit simulation and trajectory optimization of impulse thrust spacecraft and near-earth asteroid rendezvous

Liu Yunkai, Chen Danhe

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Title:	Orbit simulation and trajectory optimization of impulse thrust spacecraft and near-earth asteroid rendezvous
Keywords:	астероидная опасность импульсная тяга максимальная скорость сближения масса корабля методы оптимизации траектории моделирование орбиты предотвращение столкновений ударные космические корабли
Issue Date:	2021
Citation:	Liu Yunkai Orbit simulation and trajectory optimization of impulse thrust spacecraft and near-earth asteroid rendezvous. - Текст : электронный / Liu Yunkai, Chen Danhe // XVI Королевские чтения : междунар. молодеж. науч. конф., посвящ. 60-летию полета в космос Ю. А. Гагарина : сб. материалов : 5-7 окт. 2021 г. : в 3 т. / М-во науки и высш. образования Рос. Федерации, Самар. нац. исслед. ун-т им. С. П. Королева (Самар. ун-т) ; [науч. ред. М. А. Шлеенков]. - 2021. - Т. 1. - С. 91
URI:	http://repo.ssau.ru/jspui/handle/123456789/8715
Appears in Collections:	Королевские чтения

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